Lockheed U-2 vs. North American FJ-4 Fury
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Lockheed U-2 |
versus |
North American FJ-4 Fury |
19.2 m |
63 ft 0 in |
length |
11.1 m |
36 ft 5 in |
4.8 m |
15 ft 9 in |
height |
3.2 m |
10 ft 6 in |
32 m |
105 ft |
wingspan |
12.09 m |
39 ft 8 in |
1 × General Electric F118-101 |
engines |
1x Wright J65-W-16A |
17,000 lbf (76 kN) |
thrust per engine |
7,700 lbf |
17,000 lbf (76 kN) |
total thrust |
7,700 lbf |
18,144 kg |
40,000 lb |
MTOW |
10,750 kg |
23,700 lb |
6,090 nm |
11,278 km |
range |
3,253 km |
1,755 nm |
475 mph |
764 km/h |
cruise speed |
Mach 0.83 |
1,025 km/h |
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capacity |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.